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You searched for +publisher:"University of Cincinnati" +contributor:("Orkwis, Paul"). Showing records 1 – 11 of 11 total matches.

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University of Cincinnati

1. Heberling, Brian. A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2017, University of Cincinnati

 Computational fluid dynamics (CFD) simulations can offer a detailed view of the complex flow fields within an axial compressor and greatly aid the design process.… (more)

Subjects/Keywords: Aerospace Materials; computational fluid dynamics; turbomachinery; transonic compressor; cfd; compressor stall

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APA (6th Edition):

Heberling, B. (2017). A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623

Chicago Manual of Style (16th Edition):

Heberling, Brian. “A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor.” 2017. Masters Thesis, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623.

MLA Handbook (7th Edition):

Heberling, Brian. “A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor.” 2017. Web. 13 Nov 2019.

Vancouver:

Heberling B. A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor. [Internet] [Masters thesis]. University of Cincinnati; 2017. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623.

Council of Science Editors:

Heberling B. A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor. [Masters Thesis]. University of Cincinnati; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623


University of Cincinnati

2. Garmann, Daniel J. High-Fidelity Simulations of Transitional Flow Over Pitching Airfoils.

Degree: MS, Engineering : Aerospace Engineering, 2010, University of Cincinnati

  Presented is a high-fidelity, computational study of transitional flow over an airfoil as it is pitched up from an initial zero incidence to 40… (more)

Subjects/Keywords: Aerospace Materials; ILES; compact finite difference; implicit large eddy simulation; perching; pitching airfoils; micro air vehicle

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APA (6th Edition):

Garmann, D. J. (2010). High-Fidelity Simulations of Transitional Flow Over Pitching Airfoils. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1276955868

Chicago Manual of Style (16th Edition):

Garmann, Daniel J. “High-Fidelity Simulations of Transitional Flow Over Pitching Airfoils.” 2010. Masters Thesis, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1276955868.

MLA Handbook (7th Edition):

Garmann, Daniel J. “High-Fidelity Simulations of Transitional Flow Over Pitching Airfoils.” 2010. Web. 13 Nov 2019.

Vancouver:

Garmann DJ. High-Fidelity Simulations of Transitional Flow Over Pitching Airfoils. [Internet] [Masters thesis]. University of Cincinnati; 2010. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1276955868.

Council of Science Editors:

Garmann DJ. High-Fidelity Simulations of Transitional Flow Over Pitching Airfoils. [Masters Thesis]. University of Cincinnati; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1276955868


University of Cincinnati

3. Galbraith, Marshall Chistopher. Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil.

Degree: MS, Engineering : Aerospace Engineering, 2009, University of Cincinnati

 A laminar separation bubble is known to be detrimental to the performance of airfoils operating at low Reynolds numbers (Re < 105). With increasing interest… (more)

Subjects/Keywords: Aerospace Materials; Engineering; Large Eddy Simulation; Laminar Separation Bubble; Transitional Flow; SD7003

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APA (6th Edition):

Galbraith, M. C. (2009). Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242939414

Chicago Manual of Style (16th Edition):

Galbraith, Marshall Chistopher. “Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil.” 2009. Masters Thesis, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242939414.

MLA Handbook (7th Edition):

Galbraith, Marshall Chistopher. “Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil.” 2009. Web. 13 Nov 2019.

Vancouver:

Galbraith MC. Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil. [Internet] [Masters thesis]. University of Cincinnati; 2009. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242939414.

Council of Science Editors:

Galbraith MC. Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil. [Masters Thesis]. University of Cincinnati; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242939414


University of Cincinnati

4. Clark, Kylen D. A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2015, University of Cincinnati

 Supersonic wind tunnels are a vital aspect to the aerospace industry. Both the design and testing processes of different aerospace components often include and depend… (more)

Subjects/Keywords: Aerospace Materials; Computational Fluid Dynamics; Wind tunnels; Asymmetric Supersonic Nozzles; Test section flow; flow uniformity; Converging Diverging Nozzles

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APA (6th Edition):

Clark, K. D. (2015). A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447071393

Chicago Manual of Style (16th Edition):

Clark, Kylen D. “A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels.” 2015. Masters Thesis, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447071393.

MLA Handbook (7th Edition):

Clark, Kylen D. “A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels.” 2015. Web. 13 Nov 2019.

Vancouver:

Clark KD. A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels. [Internet] [Masters thesis]. University of Cincinnati; 2015. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447071393.

Council of Science Editors:

Clark KD. A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels. [Masters Thesis]. University of Cincinnati; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447071393


University of Cincinnati

5. Wukie, Nathan A. A Discontinuous Galerkin Method for Turbomachinery and Acoustics Applications.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2018, University of Cincinnati

 Numerical methods for computational physics have been applied for many years in the fields of turbomachinery and acoustics. The computational approach to addressing problems in… (more)

Subjects/Keywords: Aerospace Materials; High-order methods; Computational Fluid Dynamics; discontinuous Galerkin; Nonreflecting boundary conditions; Turbomachinery; Finite-elements

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APA (6th Edition):

Wukie, N. A. (2018). A Discontinuous Galerkin Method for Turbomachinery and Acoustics Applications. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543840344167045

Chicago Manual of Style (16th Edition):

Wukie, Nathan A. “A Discontinuous Galerkin Method for Turbomachinery and Acoustics Applications.” 2018. Doctoral Dissertation, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543840344167045.

MLA Handbook (7th Edition):

Wukie, Nathan A. “A Discontinuous Galerkin Method for Turbomachinery and Acoustics Applications.” 2018. Web. 13 Nov 2019.

Vancouver:

Wukie NA. A Discontinuous Galerkin Method for Turbomachinery and Acoustics Applications. [Internet] [Doctoral dissertation]. University of Cincinnati; 2018. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543840344167045.

Council of Science Editors:

Wukie NA. A Discontinuous Galerkin Method for Turbomachinery and Acoustics Applications. [Doctoral Dissertation]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543840344167045


University of Cincinnati

6. Kalagotla, Dilip. Modeling Particle Drag in Accelerating Flows with Implications for SBLI in PIV - A Numerical Analysis.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2018, University of Cincinnati

 Since its inception, Particle Image Velocimetry (PIV) has been increasingly used to measure the velocity of the flow field, especially in aerospace applications. One of… (more)

Subjects/Keywords: Aerospace Materials; Numerical modeling; Multiphase analysis; PIV; SBLI; Validation techniques; Particle drag modeling

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APA (6th Edition):

Kalagotla, D. (2018). Modeling Particle Drag in Accelerating Flows with Implications for SBLI in PIV - A Numerical Analysis. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1523630352322552

Chicago Manual of Style (16th Edition):

Kalagotla, Dilip. “Modeling Particle Drag in Accelerating Flows with Implications for SBLI in PIV - A Numerical Analysis.” 2018. Masters Thesis, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1523630352322552.

MLA Handbook (7th Edition):

Kalagotla, Dilip. “Modeling Particle Drag in Accelerating Flows with Implications for SBLI in PIV - A Numerical Analysis.” 2018. Web. 13 Nov 2019.

Vancouver:

Kalagotla D. Modeling Particle Drag in Accelerating Flows with Implications for SBLI in PIV - A Numerical Analysis. [Internet] [Masters thesis]. University of Cincinnati; 2018. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1523630352322552.

Council of Science Editors:

Kalagotla D. Modeling Particle Drag in Accelerating Flows with Implications for SBLI in PIV - A Numerical Analysis. [Masters Thesis]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1523630352322552

7. Lee, Daniel H. Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance Predictions of Low Speed and Transonic Compressor Rotors.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

 The impact blade row interactions can have on the performance of compressor rotors has been well documented. It is also well known that rotor tip… (more)

Subjects/Keywords: Aerospace Materials; unsteady; compressor; tip-vortex; blade-row interactions; upstream wakes; downstream potential effects

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APA (6th Edition):

Lee, D. H. (2013). Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance Predictions of Low Speed and Transonic Compressor Rotors. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1380620247

Chicago Manual of Style (16th Edition):

Lee, Daniel H. “Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance Predictions of Low Speed and Transonic Compressor Rotors.” 2013. Doctoral Dissertation, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1380620247.

MLA Handbook (7th Edition):

Lee, Daniel H. “Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance Predictions of Low Speed and Transonic Compressor Rotors.” 2013. Web. 13 Nov 2019.

Vancouver:

Lee DH. Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance Predictions of Low Speed and Transonic Compressor Rotors. [Internet] [Doctoral dissertation]. University of Cincinnati; 2013. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1380620247.

Council of Science Editors:

Lee DH. Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance Predictions of Low Speed and Transonic Compressor Rotors. [Doctoral Dissertation]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1380620247

8. Galbraith, Marshall C. A Discontinuous Galerkin Chimera Overset Solver.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

 This work summarizes the development of an accurate, efficient, and flexible Computational Fluid Dynamics computer code that is an improvement relative to the state of… (more)

Subjects/Keywords: Aerospace Materials; Computational Fluid Dynamics; Discontinuous Galerkin; Chimera Method; High Order Methods

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APA (6th Edition):

Galbraith, M. C. (2013). A Discontinuous Galerkin Chimera Overset Solver. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384427339

Chicago Manual of Style (16th Edition):

Galbraith, Marshall C. “A Discontinuous Galerkin Chimera Overset Solver.” 2013. Doctoral Dissertation, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384427339.

MLA Handbook (7th Edition):

Galbraith, Marshall C. “A Discontinuous Galerkin Chimera Overset Solver.” 2013. Web. 13 Nov 2019.

Vancouver:

Galbraith MC. A Discontinuous Galerkin Chimera Overset Solver. [Internet] [Doctoral dissertation]. University of Cincinnati; 2013. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384427339.

Council of Science Editors:

Galbraith MC. A Discontinuous Galerkin Chimera Overset Solver. [Doctoral Dissertation]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384427339

9. Duncan, Sean. Implementation of Slater Boundary Condition into OVERFLOW.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

 Bleed is one of the primary methods of controlling the flow within a mixed compression inlet. In this work the Slater boundary condition, first applied… (more)

Subjects/Keywords: Aerospace Materials; Bleed boundary condition; mixed compression inlet

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APA (6th Edition):

Duncan, S. (2013). Implementation of Slater Boundary Condition into OVERFLOW. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1368026265

Chicago Manual of Style (16th Edition):

Duncan, Sean. “Implementation of Slater Boundary Condition into OVERFLOW.” 2013. Masters Thesis, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1368026265.

MLA Handbook (7th Edition):

Duncan, Sean. “Implementation of Slater Boundary Condition into OVERFLOW.” 2013. Web. 13 Nov 2019.

Vancouver:

Duncan S. Implementation of Slater Boundary Condition into OVERFLOW. [Internet] [Masters thesis]. University of Cincinnati; 2013. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1368026265.

Council of Science Editors:

Duncan S. Implementation of Slater Boundary Condition into OVERFLOW. [Masters Thesis]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1368026265

10. Wukie, Nathan A. An analysis of booster tone noise using a time-linearized Navier-Stokes solver.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 This thesis details a computational investigation of tone noise generated from a booster(low-pressure compressor) in a fan test rig. The computational study consisted of sets… (more)

Subjects/Keywords: Aerospace Materials; Computational Aeroacoustics; Turbomachinery; Computational Fluid Dynamics; Acoustics; Frequency-Domain Solvers

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APA (6th Edition):

Wukie, N. A. (2016). An analysis of booster tone noise using a time-linearized Navier-Stokes solver. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458814807

Chicago Manual of Style (16th Edition):

Wukie, Nathan A. “An analysis of booster tone noise using a time-linearized Navier-Stokes solver.” 2016. Masters Thesis, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458814807.

MLA Handbook (7th Edition):

Wukie, Nathan A. “An analysis of booster tone noise using a time-linearized Navier-Stokes solver.” 2016. Web. 13 Nov 2019.

Vancouver:

Wukie NA. An analysis of booster tone noise using a time-linearized Navier-Stokes solver. [Internet] [Masters thesis]. University of Cincinnati; 2016. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458814807.

Council of Science Editors:

Wukie NA. An analysis of booster tone noise using a time-linearized Navier-Stokes solver. [Masters Thesis]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458814807

11. Garmann, Daniel J. Characterization of the vortex formation and evolution about a revolving wing using high-fidelity simulation.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

 A numerical study is conducted to examine the vortex structure and aerodynamic loading about a revolving wing in quiescent flow. The high-fidelity, implicit large eddy… (more)

Subjects/Keywords: Aerospace Materials; vortex dynamics; bio-inspired aerodynamics; large eddy simulation; revolving wings; vortex transition and breakdown; high-fidelity simulation

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APA (6th Edition):

Garmann, D. J. (2013). Characterization of the vortex formation and evolution about a revolving wing using high-fidelity simulation. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1367927773

Chicago Manual of Style (16th Edition):

Garmann, Daniel J. “Characterization of the vortex formation and evolution about a revolving wing using high-fidelity simulation.” 2013. Doctoral Dissertation, University of Cincinnati. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1367927773.

MLA Handbook (7th Edition):

Garmann, Daniel J. “Characterization of the vortex formation and evolution about a revolving wing using high-fidelity simulation.” 2013. Web. 13 Nov 2019.

Vancouver:

Garmann DJ. Characterization of the vortex formation and evolution about a revolving wing using high-fidelity simulation. [Internet] [Doctoral dissertation]. University of Cincinnati; 2013. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1367927773.

Council of Science Editors:

Garmann DJ. Characterization of the vortex formation and evolution about a revolving wing using high-fidelity simulation. [Doctoral Dissertation]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1367927773

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